Finite Element Analysis of Laminated Composite Shells of Revolutin with a Physical Non-linearity
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG14__%2F02%3A01000032" target="_blank" >RIV/60162694:G14__/02:01000032 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Finite Element Analysis of Laminated Composite Shells of Revolutin with a Physical Non-linearity
Original language description
The finite element method is applied to the determination of displacements and stresses in laminated composite shells of revolution with a physical non - linearity. The shell is modelled using a series of cylindrical or conical shell elements.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
KA - Militarism
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2002
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
19. uživatelská konference COSMOS/2002
ISBN
80-238-9614-8
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
31-36
Publisher name
TechSoft Engineering
Place of publication
Praha
Event location
Milovy
Event date
Oct 23, 2002
Type of event by nationality
CST - Celostátní akce
UT code for WoS article
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